CN109466760A - A kind of suspension shooting unmanned plane with blade hurricane globe - Google Patents
A kind of suspension shooting unmanned plane with blade hurricane globe Download PDFInfo
- Publication number
- CN109466760A CN109466760A CN201811372839.2A CN201811372839A CN109466760A CN 109466760 A CN109466760 A CN 109466760A CN 201811372839 A CN201811372839 A CN 201811372839A CN 109466760 A CN109466760 A CN 109466760A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- suspension
- blade
- main body
- force
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Abstract
The invention discloses a kind of, and the suspension with blade hurricane globe shoots unmanned plane, its structure includes unmanned plane main body, electron speed regulator, propeller, half arc air-resistance cover, umbrella shape retaining frame, fixing leg, charging socket, high-definition camera, when the skyborne unmanned plane of suspension stay, which is encountered, pushes away resistance compared with strong wind air-flow, pod can elapse inward along gas-flow resistance and follow spiral guide rod directional-rotation, to which half circumference axis of twisting is turned round by support platform, make bottom end gear and the continuous gear motion of driving rack, force-transmitting pole stretching, extension outgoing elastic force is pushed to make two sliding blocks in retainer along dedicated arc guide rail slide apart, its deformation is set to have an effect to press the spring in condensation by end end during quick sliding, more piece push rod is allowed to drive to slip off exhibition on telescopic cover plate and obstruct propeller and wind-force and separate, its normal homogeneous revolving speed is set to fly Balance unmanned plane main body center of gravity, it is ensured that unmanned plane can pinpoint suspension stay, while reducing camera lens shaking and clearly shooting to ground.
Description
Technical field
The present invention is a kind of suspension shooting unmanned plane with blade hurricane globe, belongs to aerial device field.
Background technique
Taking photo by plane is exactly so-called aerophotography, refers to that photographer carries stored program controlled manipulation by body or wireless remotecontrol is set
A kind of standby not manned vehicle, the top view then obtained from all kinds of building landscape of aerial photographing are nowadays common to navigate
It claps equipment and is commonly unmanned plane, its structure is simple, mobility strong, shooting personnel can be replaced to evade danger completely, need to clap
The narrow area taken the photograph, which is quickly walked, takes photo by plane, but also has following deficiency:
Propeller outer end without wind deflector and whole suppleness it is low, when leading to unmanned machine equipment fixed point remaining being shot in the sky,
Once being washed away by more powerful wind flow will cause propeller drive stall, can not be flown by fixed rotating speed neutrality
Make equipment center of gravity disequilibrium, causing equipment frequently to shake because of wing end can not precisely shoot, while also result in propeller
Losing axis makes unmanned plane directly crash.
Summary of the invention
In view of the deficienciess of the prior art, it is an object of the present invention to provide a kind of, the suspension with blade hurricane globe shoots nothing
It is man-machine, with solve propeller outer end without wind deflector and whole suppleness it is low, leading to unmanned machine equipment, fixed point remaining is shot in the sky
When, it will cause propeller drive stall once being washed away by more powerful wind flow, fixed rotating speed neutrality can not be passed through
Flight makes equipment center of gravity disequilibrium, and causing equipment frequently to shake because of wing end can not precisely shoot, while also result in spiral shell
Rotation paddle loses the problem of axis makes unmanned plane directly crash.
To achieve the goals above, the present invention is to realize by the following technical solutions: one kind is with blade hurricane globe
Suspension shoot unmanned plane, structure include unmanned plane main body, electron speed regulator, propeller, half arc air-resistance cover, umbrella shape shield
Frame, fixing leg, charging socket, high-definition camera, the unmanned plane bottom part body center front installation are equipped with high-definition camera
And using electrical connection, the electron speed regulator is located above four side horn of unmanned plane body outer wall in horizontal distribution, and unmanned plane
Four side horn end of body exterior is equipped with umbrella shape retaining frame and by nut thread through being fastenedly connected, and the propeller passes through bottom
Activity is entrenched in electron speed regulator top and using electrical connection, and the half arc choke, which is located at the top of umbrella shape retaining frame, fastens buckle
Connection, the fixing leg is symmetrically mounted on unmanned plane bottom part body center two sides through top layer screw hole by nut, described to fill
Electrical socket is located at unmanned plane bottom part body center right end.
As a further improvement of that present invention, the half arc air-resistance cover is by telescopic cover plate, more piece push rod, arc power transmission
Block carries slide plate, strikes out angle, pedestal, spring composition, and the telescopic cover plate is used by more piece push rod set by the two sides of surface
Flexible connection is embedded in chassis interior top layer, and chassis interior center is equipped with carrying slide plate and is fixedly connected, the arc force-transmitting block
Be embedded in inside carrying slide plate using being slidably connected, the spring is located at the left and right sides above chassis interior, and with more piece push rod
The connection of bottom buckle, the telescopic cover plate and pedestal are all semiarc shape, and there are two simultaneously mutually horizontal altogether for the arc force-transmitting block
It is symmetrically arranged at two sides inside carrying slide plate.
As a further improvement of that present invention, the arc force-transmitting block is equipped with sliding block, force-transmitting pole, in the section of the sliding block side
Centre is equipped with force-transmitting pole fastening and is fitting to connection, and the force-transmitting pole is scalable cylinder, due to being located at sliding block side so and driving cog
End is in horizontal line, and the sliding block is equal with dedicated arc guide rail width.
As a further improvement of that present invention, the carrying slide plate is by retainer, dedicated arc guide rail, rotating seat, locking stud
Composition, the retainer top surface are equipped with the equidistant arrangement locking stud that surround and are fastenedly connected, the dedicated arc guide rail anchor
It is trapped in inside retainer, and retainer side center is fitting to connection equipped with rotating seat transition, the retainer and center of inside
The dedicated arc guide rail being equipped with is integrated.
As a further improvement of that present invention, the rotating seat is by support platform, pod, half circumference axis, driving rack, spiral shell
Guide rod, shell composition are revolved, the support platform is located at interior of shell top center by top vertically fitting, and the pod passes through
Slot and spiral guide rod movable fit on the right side of shell are worn, and spiral guide rod is fastenedly connected at the top of half circumference axis by inner wall side
Outer wall, the half circumference axis top is vertically embedded into support platform bottom center, and uses interference by bottom and driving rack
Engagement is flexibly connected, and side wall is equipped with guiding snake outside the spiral guide rod, and there are two be respectively provided at the driving rack altogether
Interior of shell bottom end two sides, and the gear that the teeth being equipped with by opposite face are equipped with half circumference axis bottom is intermeshed.
As a further improvement of that present invention, the angle of striking out is by joint angle, mounting plate, link block, rotation fixing axle group
At the joint angle rotates fixing axle activity by top and is entrenched in mounting plate left and right ends, and mounting plate center of top is set
There is link block to be closely fitted into activity even, the link block is the handstand spill of fixed rotation.
Beneficial effect
A kind of suspension with blade hurricane globe of the present invention shoots unmanned plane, when the skyborne unmanned plane of suspension stay encounters
When pushing away resistance compared with strong wind air-flow, pod will elapse inward along gas-flow resistance follows the orientation rotation of spiral guide rod outer wall snake
Turn, so that half circumference axis of twisting turns round by support platform and reduces own load, engages bottom end gear continuously with driving rack
Movement generates power after rubbing using respective side wall tooth, force-transmitting pole stretching, extension outgoing elastic force is pushed to make to be applied in retainer
Two sliding blocks are along dedicated arc guide rail opposite direction slide apart, to be pressed in condensation during quick sliding by end end
Spring makes its deformation have an effect, and allows more piece push rod to drive to slip off exhibition on telescopic cover plate and obstruct propeller and wind-force and separate, makes it
Normal homogeneous revolving speed flies to balance the center of gravity of unmanned plane main body, it is ensured that unmanned plane can pinpoint suspension stay, while can subtract again
Tiny lens shaking clearly shoots ground.
Detailed description of the invention
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other feature of the invention,
Objects and advantages will become more apparent upon:
Fig. 1 is a kind of structural schematic diagram of the suspension shooting unmanned plane with blade hurricane globe of the present invention；
Fig. 2 is the action schematic diagram of half arc air-resistance cover of the invention.
Fig. 3 is the external structure schematic diagram of half arc air-resistance cover of the invention；
Fig. 4 is the schematic diagram of internal structure of half arc air-resistance cover of the invention；
Fig. 5 is the structural schematic diagram of arc force-transmitting block of the present invention；
Fig. 6 is the structural schematic diagram of present invention carrying slide plate；
Fig. 7 is the schematic diagram of internal structure of rotating seat of the present invention；
Fig. 8 is the structural schematic diagram that the present invention strikes out angle；
In figure: unmanned plane main body -1, propeller -3, half arc air-resistance cover -4, umbrella shape retaining frame -5, is consolidated electron speed regulator -2
Determine stabilizer blade -6, charging socket -7, high-definition camera -8, telescopic cover plate -41, more piece push rod -42, arc force-transmitting block -43, carrying
Slide plate -44 strikes out angle -45, pedestal -46, spring -47, sliding block -431, force-transmitting pole -432, retainer -441, dedicated arc guide rail -
442, rotating seat -443, locking stud -444, support platform -4431, pod -4432, half circumference axis -4433, driving rack -
4434, spiral guide rod -4435, shell -4436, joint angle -451, mounting plate -452, link block -453, rotation fixing axle -
454。
Specific embodiment
To be easy to understand the technical means, the creative features, the aims and the efficiencies achieved by the present invention, below with reference to
Specific embodiment, the present invention is further explained.
Fig. 1-Fig. 8 is please referred to, the present invention provides a kind of suspension shooting unmanned plane with blade hurricane globe, and structure includes
Unmanned plane main body 1, electron speed regulator 2, propeller 3, half arc air-resistance cover 4, umbrella shape retaining frame 5, fixing leg 6, charging socket 7,
High-definition camera 8,1 bottom center front end of the unmanned plane main body installation are equipped with high-definition camera 8 and using electrical connection, the electricity
Sub- governor 2 is located above 1 outer wall of unmanned plane main body, four side horn in horizontal distribution, and 1 four side horns of outside of unmanned plane main body
End is equipped with umbrella shape retaining frame 5 and by nut thread through being fastenedly connected, and the propeller 3 is entrenched in electronics by bottom activity
2 top of governor simultaneously uses electrical connection, and the half arc air-resistance cover 4, which is located at the top of umbrella shape retaining frame 5, fastens buckle connection, described solid
Determine stabilizer blade 6 and 1 bottom center two sides of unmanned plane main body are symmetrically mounted on through top layer screw hole by nut, the charging socket 7 is set
In 1 bottom center right end of unmanned plane main body.
As a further improvement of that present invention, the half arc air-resistance cover 4 is by telescopic cover plate 41, more piece push rod 42, arc
Force-transmitting block 43, carrying slide plate 44 strike out angle 45, pedestal 46, the composition of spring 47, and the telescopic cover plate 41 passes through surface two sides institute
If more piece push rod 42 be embedded in 46 inner top layer of pedestal using being flexibly connected, and 46 center of inside of pedestal is equipped with carrying slide plate 44
It is fixedly connected, the arc force-transmitting block 43 is embedded in inside carrying slide plate 44 using being slidably connected, and the spring 47 is located at pedestal
It at left and right sides of 46 inner uppers, and is connect with 42 bottom buckle of more piece push rod, above-mentioned more piece push rod 42 is located at telescopic cover plate 41
Inner surface two sides, the purpose is to be avoided while being condensed stretching routine together with telescopic cover plate 41 to its height limitation
Power collision is elongated and loosens bottom inner end.
As a further improvement of that present invention, the arc force-transmitting block 43 is equipped with sliding block 431, force-transmitting pole 432, the sliding block
431 side section centers are equipped with the fastening of force-transmitting pole 432 and are fitting to connection, above-mentioned since force-transmitting pole is scalable cylinder, by cunning
Block 431 is that carrier can directly deeply be connect to 4436 inside of shell with driving rack 4434, when the half circumference driving transmission of axis 4433
Quickly it will accelerate 431 sliding speed of sliding block by elastic force after rack gear 4434.
As a further improvement of that present invention, the carrying slide plate 44 is by retainer 441, dedicated arc guide rail 442, rotating seat
443, locking stud 444 forms, and 441 top surface of retainer is equipped with the equidistant arrangement locking stud 444 that surround and is fastenedly connected,
442 fixed swage of dedicated arc guide rail is located inside retainer 441, and 441 side center of retainer is equipped with 443 mistake of rotating seat
Cross fitting connection, above-mentioned retainer 441 sets that there are four locking studs 444 can be fixedly attached in 46 inside of pedestal by top
Centre.
As a further improvement of that present invention, the rotating seat 443 is by support platform 4431, pod 4432, half circumference axis
4433, driving rack 4434, spiral guide rod 4435, shell 4436 form, and the support platform 4431 passes through top vertically fitting
It is located at 4436 inner upper of shell center, the pod 4432 is through 4436 right side slot of shell and 4435 gap of spiral guide rod
It is chimeric, and spiral guide rod 4435 is fastenedly connected by inner wall side in half circumference 4433 top exterior walls of axis, the half circumference axis
4433 tops are vertically embedded into 4431 bottom center of support platform, and engage work using interference with driving rack 4434 by bottom
Dynamic connection, the snake that above-mentioned 4435 outer wall of spiral guide rod is equipped with is to allow pod 4432 by wind drive along exclusive conduit
Passage, making spiral guide rod 4435, operating avoids driving in the wrong direction clockwise, and the effect of half circumference axis 4433 is had enough to meet the need from back and forth half
When dynamic can Traction Drive rack gear 4434 slidably reciprocate.
As a further improvement of that present invention, it is described strike out angle 45 by joint angle 451, mounting plate 452, link block 453, turn
Dynamic fixing axle 454 forms, and the joint angle 451 rotates 454 activity of fixing axle by top and is entrenched in mounting plate 452 or so two
End, and 452 center of top of mounting plate is equipped with link block 453 and is closely fitted into flexible connection, above-mentioned joint angle 451 is solid by rotation
Dead axle 454 rotates angle modulation width, mainly allows half arc air-resistance cover 4 being mounted in umbrella shape retaining frame 5 can be with dismounting and change, or peace
On other unmanned machine equipments with existing unmanned plane same size.
Working principle:
It is connect by internal wireless remotecontrol program mounted with external control equipment by unmanned plane main body 1, using
External control equipment, which controls it, makes electron speed regulator 2 drive propeller 3 quickly to overturn with electricity output, thus by propeller 3
The climbing power quickly generated when overturning drives unmanned plane main body 1 to rise, and the air of front is then applied pressure again and is allowed to quick
Flowing backward and generating forward thrust pushes unmanned plane main body 1 to advance, then strikes out 45 internal joint of angle folder by 46 bottom end of pedestal
Angle 451 is fixedly attached to 5 top of umbrella shape retaining frame by rotation 454 angle modulation of fixing axle, by half arc air-resistance cover 4, in pod
4432 by outer Wind power propelling when will immediately press inward, it is then sliding along the snakelike thread orientation of 4432 outer wall of pod
It is dynamic, so that it is drawn half circumference axis 4433 and consolidates lower holding vertical scrolling in the support platform 4431 of 4436 inner upper of shell, from
And generated after going into overdrive to allow bottom end gear and the continuous gear motion of driving rack 4434 to rub using respective side wall tooth
Power drives force-transmitting pole 432 to be upheld outward and allows two sliding blocks 431 being applied in 441 two sides of retainer along dedicated arc guide rail
Then 442 arc-shaped shape opposite direction slide aparts utilize the generated impulse force impact spring 47 in quick sliding of sliding block 431, this
When in compression shape spring 47 will immediately deformation have an effect to touch more piece push rod 42 and drive and slip off exhibition on telescopic cover plate 41, borrow
This separates propeller 3 and peripheral wind-force moment barrier, and propeller 3 is allowed to keep normal homogeneous revolving speed rotation weighing apparatus unmanned plane main body 1
Whole center of gravity, so that unmanned plane is pinpointed suspension stay, at the same avoid high-definition camera 8 shake, clearly to clap ground
It takes the photograph.
The present invention is combined with each other by above-mentioned component, when the skyborne unmanned plane of suspension stay is encountered compared with strong wind air-flow
When pushing away resistance, pod 4432 will elapse inward along gas-flow resistance follows 4435 outer wall snake directional-rotation of spiral guide rod,
Reduce own load to which half circumference axis 4433 of twisting is turned round by support platform 4431, makes bottom end gear and driving rack 4434
Continuous gear motion generates power after rubbing using respective side wall tooth, and pushing force-transmitting pole 432 to stretch outgoing elastic force makes to run through
Two sliding blocks 431 in retainer 441 are along the opposite slide apart of dedicated arc guide rail 442, thus during quick sliding
Pressing the spring 47 in condensation by end end makes its deformation have an effect, and allows more piece push rod 42 to drive on telescopic cover plate 41 and slips off exhibition
Propeller 3 and wind-force barrier are separated, make the flight of its normal homogeneous revolving speed to balance the center of gravity of unmanned plane main body 1, it is ensured that nobody
Machine can pinpoint suspension stay, while can reduce camera lens shaking again and clearly shoot to ground.
The above shows and describes the basic principles and main features of the present invention and the advantages of the present invention, for this field skill
For art personnel, it is clear that invention is not limited to the details of the above exemplary embodiments, and without departing substantially from spirit of the invention or
In the case where essential characteristic, the present invention can be realized in other specific forms.Therefore, in all respects, should all incite somebody to action
Embodiment regards exemplary as, and is non-limiting, the scope of the present invention by appended claims rather than on state
Bright restriction, it is intended that including all changes that fall within the meaning and scope of the equivalent elements of the claims in the present invention
It is interior.Any reference signs in the claims should not be construed as limiting the involved claims.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiments being understood that.
Claims (6)
1. a kind of suspension with blade hurricane globe shoots unmanned plane, structure includes unmanned plane main body (1), electron speed regulator
(2), propeller (3), half arc air-resistance cover (4), umbrella shape retaining frame (5), fixing leg (6), charging socket (7), high-definition camera
(8), it is characterised in that:
Unmanned plane main body (1) the bottom center front end installation is equipped with high-definition camera (8) and using electrical connection, the electronics tune
Fast device (2) is located above four side horn of unmanned plane main body (1) outer wall in horizontal distribution, and the external four side machines of unmanned plane main body (1)
Arm end is equipped with umbrella shape retaining frame (5) and by nut thread through being fastenedly connected, and the propeller (3) is chimeric by bottom activity
On electron speed regulator (2) top and using electrical connection, it is embedding that the half arc air-resistance cover (4) is located at fastening at the top of umbrella shape retaining frame (5)
Button connection, the fixing leg (6) are symmetrically mounted on unmanned plane main body (1) bottom center two through top layer screw hole by nut
Side, the charging socket (7) are located at unmanned plane main body (1) bottom center right end.
2. a kind of suspension with blade hurricane globe according to claim 1 shoots unmanned plane, it is characterised in that: described half
Arc air-resistance cover (4) by telescopic cover plate (41), more piece push rod (42), arc force-transmitting block (43), carrying slide plate (44), strike out angle
(45), pedestal (46), spring (47) composition, the telescopic cover plate (41) are adopted by more piece push rod (42) set by the two sides of surface
It is embedded in pedestal (46) inner top layer with flexible connection, and pedestal (46) center of inside is equipped with carrying slide plate (44) and is fixedly connected,
The arc force-transmitting block (43) is embedded in carrying slide plate (44) inside using being slidably connected, and the spring (47) is located at pedestal (46)
At left and right sides of inner upper, and it is connect with more piece push rod (42) bottom buckle.
3. a kind of suspension with blade hurricane globe according to claim 2 shoots unmanned plane, it is characterised in that: the arc
Shape force-transmitting block (43) is equipped with sliding block (431), force-transmitting pole (432), and sliding block (431) the side section center is equipped with force-transmitting pole
(432) fastening is fitting to connection.
4. a kind of suspension with blade hurricane globe according to claim 2 shoots unmanned plane, it is characterised in that: described to hold
It carries slide plate (44) to be made of retainer (441), dedicated arc guide rail (442), rotating seat (443), locking stud (444), the guarantor
It holds frame (441) top surface to be fastenedly connected equipped with equidistant around arrangement locking stud (444), the dedicated arc guide rail (442) is admittedly
It is internal that fixed recess is located at retainer (441), and retainer (441) side center is fitting to connection equipped with rotating seat (443) transition.
5. a kind of suspension with blade hurricane globe according to claim 4 shoots unmanned plane, it is characterised in that: the rotation
Swivel base (443) is by support platform (4431), pod (4432), half circumference axis (4433), driving rack (4434), spiral guide rod
(4435), shell (4436) forms, and the support platform (4431) is located on shell (4436) inside by top vertically fitting
Fang Zhongyang, the pod (4432) run through slot and spiral guide rod (4435) movable fit on the right side of shell (4436), and spiral
Guide rod (4435) is fastenedly connected at the top of half circumference axis (4433) top exterior walls, half circumference axis (4433) by inner wall side
It is vertically embedded into support platform (4431) bottom center, and activity is engaged using interference with driving rack (4434) by bottom and is connected
It connects.
6. a kind of suspension with blade hurricane globe according to claim 2 shoots unmanned plane, it is characterised in that: the hook
Pin angle (45) is made of joint angle (451), mounting plate (452), link block (453), rotation fixing axle (454), the joint
Angle (451) rotates fixing axle (454) activity by top and is entrenched in mounting plate (452) left and right ends, and mounting plate (452) pushes up
Portion center is equipped with link block (453) closely chimeric flexible connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811372839.2A CN109466760A (en) | 2018-11-19 | 2018-11-19 | A kind of suspension shooting unmanned plane with blade hurricane globe |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811372839.2A CN109466760A (en) | 2018-11-19 | 2018-11-19 | A kind of suspension shooting unmanned plane with blade hurricane globe |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109466760A true CN109466760A (en) | 2019-03-15 |
Family
ID=65672688
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811372839.2A Withdrawn CN109466760A (en) | 2018-11-19 | 2018-11-19 | A kind of suspension shooting unmanned plane with blade hurricane globe |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109466760A (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110254699A (en) * | 2019-06-28 | 2019-09-20 | 江苏大成航空科技有限公司 | A kind of agricultural plant protection unmanned plane rotor protective device |
| CN110871890A (en) * | 2020-01-20 | 2020-03-10 | 天津微深科技有限公司 | Four rotor unmanned aerial vehicle |
| CN111183830A (en) * | 2020-03-24 | 2020-05-22 | 崔德念 | Automatic windproof system for greenhouse |
| CN111959804A (en) * | 2020-08-26 | 2020-11-20 | 深圳市天同玩具有限公司 | Anti-deviation protection device for aerial photography |
| CN112607019A (en) * | 2020-12-14 | 2021-04-06 | 金肯职业技术学院 | Windproof type suspension shooting unmanned aerial vehicle and stable shooting method |
| CN113371196A (en) * | 2021-07-15 | 2021-09-10 | 吉林建筑大学 | High remote sensing survey and drawing unmanned aerial vehicle of security |
| CN114264698A (en) * | 2021-12-14 | 2022-04-01 | 石家庄东方热电热力工程有限公司 | Photovoltaic power generation component hot spot fault point addressing device |
| CN114571931A (en) * | 2022-04-24 | 2022-06-03 | 浙江大学 | Amphibious unmanned aerial vehicle |
| CN116750227A (en) * | 2023-07-13 | 2023-09-15 | 深圳市畅天游智能科技有限公司 | Portable multi-rotor folding unmanned aerial vehicle |
| CN117146133A (en) * | 2023-11-01 | 2023-12-01 | 太原市水资源管理保护中心 | Remote sensing water conservancy facility deformation monitoring devices |
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2018
- 2018-11-19 CN CN201811372839.2A patent/CN109466760A/en not_active Withdrawn
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110254699A (en) * | 2019-06-28 | 2019-09-20 | 江苏大成航空科技有限公司 | A kind of agricultural plant protection unmanned plane rotor protective device |
| CN110871890A (en) * | 2020-01-20 | 2020-03-10 | 天津微深科技有限公司 | Four rotor unmanned aerial vehicle |
| CN111183830A (en) * | 2020-03-24 | 2020-05-22 | 崔德念 | Automatic windproof system for greenhouse |
| CN111959804A (en) * | 2020-08-26 | 2020-11-20 | 深圳市天同玩具有限公司 | Anti-deviation protection device for aerial photography |
| CN111959804B (en) * | 2020-08-26 | 2021-05-28 | 苏州市大智无疆智能科技有限公司 | Anti-deviation protection device for aerial photography |
| CN112607019A (en) * | 2020-12-14 | 2021-04-06 | 金肯职业技术学院 | Windproof type suspension shooting unmanned aerial vehicle and stable shooting method |
| CN113371196A (en) * | 2021-07-15 | 2021-09-10 | 吉林建筑大学 | High remote sensing survey and drawing unmanned aerial vehicle of security |
| CN114264698A (en) * | 2021-12-14 | 2022-04-01 | 石家庄东方热电热力工程有限公司 | Photovoltaic power generation component hot spot fault point addressing device |
| CN114571931A (en) * | 2022-04-24 | 2022-06-03 | 浙江大学 | Amphibious unmanned aerial vehicle |
| CN116750227A (en) * | 2023-07-13 | 2023-09-15 | 深圳市畅天游智能科技有限公司 | Portable multi-rotor folding unmanned aerial vehicle |
| CN116750227B (en) * | 2023-07-13 | 2024-01-12 | 深圳市畅天游智能科技有限公司 | Portable multi-rotor folding unmanned aerial vehicle |
| CN117146133A (en) * | 2023-11-01 | 2023-12-01 | 太原市水资源管理保护中心 | Remote sensing water conservancy facility deformation monitoring devices |
| CN117146133B (en) * | 2023-11-01 | 2024-01-02 | 太原市水资源管理保护中心 | Remote sensing water conservancy facility deformation monitoring devices |
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Application publication date: 20190315 |